Development of Algorithms for Integration and Reconfiguration of the Flight Control System and Interfaces

A. V. Efremov; M. S. Tyaglik; A. S. Tyaglik; I. Kh. Irgaleev

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Development of Algorithms for Integration and Reconfiguration of the Flight Control System and Interfaces

机译：用于集成和重新配置飞行控制系统和接口的算法的开发

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摘要

The integration potentiality is considered for the flight control system and interface algorithms to provide the flight accuracy and safety of highly augmented aircraft in the case of low maximum elevator rate limit and in the case of failures causing its sharp decrease.

机译：在最大电梯速率限制的情况下，在最大电梯速率限制的情况下，考虑了飞行控制系统和接口算法的集成潜力，以提供高度增强飞机的飞行精度和安全性。

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来源
《Russian Aeronautics》 |2018年第3期|共5页
作者
A. V. Efremov; M. S. Tyaglik; A. S. Tyaglik; I. Kh. Irgaleev;
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作者单位

Moscow Aviation Institute (National Research University);

Moscow Aviation Institute (National Research University);

Moscow Aviation Institute (National Research University);

Moscow Aviation Institute (National Research University);

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原文格式 PDF
正文语种 eng
中图分类航空;
关键词
pilot–aircraft system; semiautomatic control; manual control; predictive display;

机译：飞行员系统;半自动控制;手动控制;预测显示;

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专利

1. Development of Algorithms for Integration and Reconfiguration of the Flight Control System and Interfaces [J] . A. V. Efremov, M. S. Tyaglik, A. S. Tyaglik, Russian Aeronautics . 2018,第3期

机译：用于集成和重新配置飞行控制系统和接口的算法的开发
2. Multimodel-based flight control system reconfiguration control in the presence of input constraints [J] . Yuying GUO, Bin JIANG, Yufei XU 控制理论与应用：英文版 . 2010,第004期

机译：存在输入约束的基于多模型的飞行控制系统重构控制
3. Multimodel-based flight control system reconfiguration control in the presence of input constraints [J] . Yuying GUO, Bin JIANG, Yufei XU 控制理论与应用（英文版） . 2010,第004期

机译：存在输入约束的基于多模型的飞行控制系统重构控制
4. THE HELICOPTER MATH MODEL INTEGRATION WITH THE SIMULINK SOFTWARE PACKAGE, AND RESEARCH FOR THE MI-172 HELICOPTER AUTOMATIC FLIGHT CONTROL SYSTEM ALGORITHMS DEVELOPMENT [C] . Sergei Y. Esaulov, Alexander P. Vaintrub, Tatiana V. Ivakova European rotorcraft forum;ERF33 . 2007

机译：集成了SIMULINK软件包的直升机数学模型，以及MI-172直升机自动飞行控制系统算法开发的研究
5. A new approach to the flight control system reconfiguration following a battle damage and/or a generic failure on a control surface. [D] . Napolitano, Marcello Rosario. 1989

机译：战斗损坏和/或控制面上发生一般性故障后，重新配置飞行控制系统的新方法。
6. Development of Wheel Pressure Control Algorithm for Electronic Stability Control (ESC) System of Commercial Trucks [O] . Minjun Seo, Changhee Yoo, Sang-Shin Park, 2018

机译：商用车电子稳定控制系统轮压控制算法的开发
7. Applications of eigenstructure assignment to design of robust mimo decoupling controllers and to reconfiguration algorithms for damaged flight control. [O] . Gavito Valentin F. Jr. 1986

机译：本征结构分配在鲁棒的mimo解耦控制器设计和受损飞行控制的重新配置算法中的应用。
8. Applications of Eigenstructure Assignment to Design of Robust MIMO (Multi Input Multi Output) Decoupling Controllers and to Reconfiguration Algorithms for Damaged Flight Control Systems [R] . Gavito, V. F. 1986

机译：特征结构分配在鲁棒mImO（多输入多输出）解耦控制器设计中的应用及损伤飞行控制系统的重构算法

Development of Algorithms for Integration and Reconfiguration of the Flight Control System and Interfaces

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